Missile jet vane control system and method
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United States of America Patent
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Sep 15, 1998
Grant Date -
N/A
app pub date -
May 26, 1995
filing date -
May 26, 1995
priority date (Note) -
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Abstract
A jet vane control system and method for a missile in which the system is compact, rugged, lightweight and detachably connected to the aft end of a missile. The system provides for very quick pitch over and roll control during launch. The system then detaches from the missile so as not to burden the missile during its flight to target. The vanes of the system are divided into quadrants, each having its own, mounting support and gear train assembly. Each vane is also connected through a, detachable coupling to the steering control system of the missile such that actuation of the steering control system simultaneously actuates the jet vane control system.
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